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w j bannink

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CiltDetermination of the Position of a Shock Wave from Pittot Tube ExperimentsW.J. Bannink, C. Nebbeling, Delft University of Technology, Department of Aeronautical Engineering

Determination of the Position of a Shock Wave from Pittot Tube Experiments

W.J. Bannink, C. Nebbeling, Delft University of Technology, Department of Aeronautical Engineering · Yayınevi bilinmiyor

Sayfa sayısı yok · 1966

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Air flowOn the Numerical Computation of the Supersonic Flow Field about Blunted Cones at Small Angles of IncidenceL. L. van Dommelen, W. J. Bannink

On the Numerical Computation of the Supersonic Flow Field about Blunted Cones at Small Angles of Incidence

L. L. van Dommelen, W. J. Bannink · Yayınevi bilinmiyor

110 sayfa · 1976

Air flow

CiltExperimental and Computational Study of a Blunt Cylinder-flare Model in High Supersonic FlowE. M. Houtman, W. J. Bannink, B. H. Timmerman

Experimental and Computational Study of a Blunt Cylinder-flare Model in High Supersonic Flow

E. M. Houtman, W. J. Bannink, B. H. Timmerman · Yayınevi bilinmiyor

33 sayfa · 1995

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CiltNote on the Separated Flow Over a Delta Wing at High Subsonic and Transonic SpeedsJ.A. Möller, W.J. Bannink, P.G. Bakker, Delft University of Technology, Department of Aerospace Engineering

Note on the Separated Flow Over a Delta Wing at High Subsonic and Transonic Speeds

J.A. Möller, W.J. Bannink, P.G. Bakker, Delft University of Technology, Department of Aerospace Engineering · Yayınevi bilinmiyor

Sayfa sayısı yok · 1984

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CiltInvestigation of the Vortex Flow Over a Sharp-edged Delta Wing in the Transonic Speed RegimeW. J. Bannink, E. M. Houtman, S. P. Ottochian

Investigation of the Vortex Flow Over a Sharp-edged Delta Wing in the Transonic Speed Regime

W. J. Bannink, E. M. Houtman, S. P. Ottochian · Yayınevi bilinmiyor

63 sayfa · 1989

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CiltOn the Structure of the Potential Flow Field Near Conical Stagnation Points in Supersonic FlowP. G. Bakker, W. J. Bannink, John William Reyn, Technische Hogeschool. Luchtvaart- en ruimtevaarttechniek

On the Structure of the Potential Flow Field Near Conical Stagnation Points in Supersonic Flow

P. G. Bakker, W. J. Bannink, John William Reyn, Technische Hogeschool. Luchtvaart- en ruimtevaarttechniek · Yayınevi bilinmiyor

40 sayfa · 1980

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CiltAn Experimental Investigation of the Expansion Flow Field Over a Delta Wing at Supersonic SpeedW. J. Bannink, C. Nebbeling

An Experimental Investigation of the Expansion Flow Field Over a Delta Wing at Supersonic Speed

W. J. Bannink, C. Nebbeling · Yayınevi bilinmiyor

40 sayfa · 1971

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CiltReview of Local Inclination Methods in Hypersonics and ApplicationsL. M. G. Walpot, W. J. Bannink, P. G. Bakker, Delft University of Technology. Faculty of Aerospace Engineering

Review of Local Inclination Methods in Hypersonics and Applications

L. M. G. Walpot, W. J. Bannink, P. G. Bakker, Delft University of Technology. Faculty of Aerospace Engineering · Yayınevi bilinmiyor

28 sayfa · 1996

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CiltThe Calibration and Measuring Procedure of a Five-hole Hemispherical Head Probe in Compressible FlowE. M. Houtman, W. J. Bannink

The Calibration and Measuring Procedure of a Five-hole Hemispherical Head Probe in Compressible Flow

E. M. Houtman, W. J. Bannink · Yayınevi bilinmiyor

26 sayfa · 1989

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CiltNumerical Solution of Transonic Normal Shock Wave-boundary Layer Interaction Using the Bohning-Zierep ModelB. Koren, W. J. Bannink, Technische Hogeschool. Afdeling der Luchtvaart- en Ruimtevaarttechniek

Numerical Solution of Transonic Normal Shock Wave-boundary Layer Interaction Using the Bohning-Zierep Model

B. Koren, W. J. Bannink, Technische Hogeschool. Afdeling der Luchtvaart- en Ruimtevaarttechniek · Yayınevi bilinmiyor

17 sayfa · 1984

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CiltFestip AerothermodynamicsW. J. Bannink, P. G. Bakker, E. M. Houtman, Delft University of Technology. Faculty of Aerospace Engineering

Festip Aerothermodynamics

W. J. Bannink, P. G. Bakker, E. M. Houtman, Delft University of Technology. Faculty of Aerospace Engineering · Yayınevi bilinmiyor

24 sayfa · 1997

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CiltA High-speed Surface Reflective Visualization System for the Study of Vortex Breakdown Over a Delta WingS. R. Donohoe

A High-speed Surface Reflective Visualization System for the Study of Vortex Breakdown Over a Delta Wing

S. R. Donohoe · Yayınevi bilinmiyor

Sayfa sayısı yok · 1994

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CiltSurface Flow Visualization of a Glancing Shock-wave/boundary-layer InteractionB. W. van Oudheusden, C. Nebbeling, W. J. Bannink

Surface Flow Visualization of a Glancing Shock-wave/boundary-layer Interaction

B. W. van Oudheusden, C. Nebbeling, W. J. Bannink · Yayınevi bilinmiyor

64 sayfa · 1994

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CiltFlow Visualization Study of High Supersonic Flow Past a Blunt Cylinder-cone Flare BodyP. G. Bakker, W. J. Bannink

Flow Visualization Study of High Supersonic Flow Past a Blunt Cylinder-cone Flare Body

P. G. Bakker, W. J. Bannink · Yayınevi bilinmiyor

11 sayfa · 1994

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CiltExperimental and Theoretical Study of a Progressive Cavity PumpD. Appleby

Experimental and Theoretical Study of a Progressive Cavity Pump

D. Appleby · Yayınevi bilinmiyor

305 sayfa · 1994

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CiltConical Stagnation Points in the Supersonic Flow Around Slender Circular Cones at IncidenceP. G. Bakker, W. J. Bannink, Delft University of Technology, Department of Aeronautical Engineering

Conical Stagnation Points in the Supersonic Flow Around Slender Circular Cones at Incidence

P. G. Bakker, W. J. Bannink, Delft University of Technology, Department of Aeronautical Engineering · Yayınevi bilinmiyor

53 sayfa · 1974

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CiltPreliminary Study of a Plug Nozzle Model in Supersonic FlowW. J. Bannink, E. M. Houtman, M. M. J. Schoones

Preliminary Study of a Plug Nozzle Model in Supersonic Flow

W. J. Bannink, E. M. Houtman, M. M. J. Schoones · Yayınevi bilinmiyor

31 sayfa · 1998

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CiltComputational Study of Support Influence on Base Flow of a Model in Supersonic FlowH. B. A. Ottens

Computational Study of Support Influence on Base Flow of a Model in Supersonic Flow

H. B. A. Ottens · Yayınevi bilinmiyor

Sayfa sayısı yok · 2001

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CiltInvestigation on the Flow Field on the Expansion Side of a Delta Wing with Supersonic Leading EdgesW.J. Bannink, C. Nebbeling, J.W. Reyn, Delft University of Technology. Department of Aerospace Engineering

Investigation on the Flow Field on the Expansion Side of a Delta Wing with Supersonic Leading Edges

W.J. Bannink, C. Nebbeling, J.W. Reyn, Delft University of Technology. Department of Aerospace Engineering · Yayınevi bilinmiyor

Sayfa sayısı yok · 1965

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Air flowExperimental Investigation of the Supersonic Flow Field about a Slender Cone at High IncidencesC. Nebbeling, W. J. Bannink

Experimental Investigation of the Supersonic Flow Field about a Slender Cone at High Incidences

C. Nebbeling, W. J. Bannink · Yayınevi bilinmiyor

112 sayfa · 1976

Air flow